JP2018070141A5 - - Google Patents

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Publication number
JP2018070141A5
JP2018070141A5 JP2017152114A JP2017152114A JP2018070141A5 JP 2018070141 A5 JP2018070141 A5 JP 2018070141A5 JP 2017152114 A JP2017152114 A JP 2017152114A JP 2017152114 A JP2017152114 A JP 2017152114A JP 2018070141 A5 JP2018070141 A5 JP 2018070141A5
Authority
JP
Japan
Prior art keywords
fuselage barrel
butt joint
section
stringer
main section
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2017152114A
Other languages
English (en)
Japanese (ja)
Other versions
JP2018070141A (ja
JP7012483B2 (ja
Filing date
Publication date
Priority claimed from US15/258,919 external-priority patent/US10308342B2/en
Application filed filed Critical
Publication of JP2018070141A publication Critical patent/JP2018070141A/ja
Publication of JP2018070141A5 publication Critical patent/JP2018070141A5/ja
Application granted granted Critical
Publication of JP7012483B2 publication Critical patent/JP7012483B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2017152114A 2016-09-07 2017-08-07 胴体バレルに対する損傷を修理する方法並びに関連装置及びシステム Active JP7012483B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/258,919 2016-09-07
US15/258,919 US10308342B2 (en) 2016-09-07 2016-09-07 Method of repairing damage to fuselage barrel and associated apparatus and system

Publications (3)

Publication Number Publication Date
JP2018070141A JP2018070141A (ja) 2018-05-10
JP2018070141A5 true JP2018070141A5 (zh) 2020-09-17
JP7012483B2 JP7012483B2 (ja) 2022-01-28

Family

ID=59315470

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2017152114A Active JP7012483B2 (ja) 2016-09-07 2017-08-07 胴体バレルに対する損傷を修理する方法並びに関連装置及びシステム

Country Status (5)

Country Link
US (2) US10308342B2 (zh)
EP (1) EP3293105B1 (zh)
JP (1) JP7012483B2 (zh)
CN (1) CN107792390B (zh)
CA (1) CA2974245C (zh)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
FR3089946B1 (fr) * 2018-12-18 2021-01-08 Airbus Operations Sas structure d’un FUSELAGE D’UN aeronef présentant un panneau renforcé par un treillis
US11427351B2 (en) 2019-12-06 2022-08-30 The Boeing Company Carrier and operational frame system and methods of assembling a structure
EP3978358A1 (en) 2020-09-30 2022-04-06 The Boeing Company Aircraft fuselage longitudinal splice for joining half barrel fuselage sections and other spliced fuselage sections
NL2027402B1 (en) * 2021-01-26 2022-08-19 Boeing Co Aircraft assembly formed of mating half barrel sections and the method of assembling the same
US11801576B2 (en) 2020-11-18 2023-10-31 The Boeing Company Aircraft assembly formed of mating half barrel sections and the method of assembling the same
US11919617B2 (en) 2020-12-17 2024-03-05 The Boeing Company Circumferential lap splices for sections of fuselage

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
US6849150B1 (en) * 2001-01-16 2005-02-01 Lockheed Martin Corporation System and method of forming structural assemblies with 3-D woven joint pre-forms
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
FR2901246B1 (fr) * 2006-05-19 2008-06-20 Airbus France Sas Procede de reparation d'une zone endommagee d'un fuselage d'aeronef
US7871040B2 (en) 2006-11-10 2011-01-18 The Boeing Company Composite aircraft structures with hat stiffeners
US8047469B2 (en) * 2008-03-01 2011-11-01 The Boeing Company Airframe attachment fitting
US7967250B2 (en) * 2008-05-12 2011-06-28 EMBRAER—Empresa Brasileira de Aeronáutica Hybrid aircraft fuselage structural components and methods of making same
DE102009009491A1 (de) * 2009-02-18 2010-09-09 Airbus Deutschland Gmbh Verfahren zum Herstellen eines Schalenkörpers
FR2953812B1 (fr) * 2009-12-11 2012-09-07 Airbus Operations Sas Procede de reparation d'un fuselage d'aeronef
ES2395604B1 (es) 2010-10-29 2013-12-26 Airbus Operations, S.L. Reparación interior doblada.
US8567722B2 (en) * 2010-12-15 2013-10-29 The Boeing Company Splice and associated method for joining fuselage sections
US8616500B2 (en) * 2011-03-04 2013-12-31 The Boeing Company Diamond shaped window for composite and/or metallic airframe
US8844108B2 (en) * 2011-07-12 2014-09-30 The Boeing Company Large area repair of composite aircraft
US8914979B2 (en) * 2011-07-21 2014-12-23 Spirit AcroSystems, Inc. System and method for assembling aircraft components
US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
US8939406B2 (en) * 2012-07-02 2015-01-27 The Boeing Company Joining composite fuselage sections along window belts
US8985512B1 (en) * 2012-09-21 2015-03-24 The Boeing Company Aircraft, fuselages, and associated methods
US8960606B2 (en) 2012-10-31 2015-02-24 The Boeing Company Circumference splice for joining shell structures
GB2517954B (en) * 2013-09-05 2018-07-04 Airbus Operations Ltd Repair of a damaged composite aircraft wing
EP2873620B1 (en) 2013-11-14 2018-05-16 Airbus Operations GmbH Repair method for fuselage components of aircraft or spacecraft
FR3037558B1 (fr) * 2015-06-19 2017-05-26 Airbus Operations Sas Procede de fabrication d'un panneau de fuselage par surmoulage et panneau de fuselage ainsi obtenu

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